Cessna CE-335

A lightweight unpressurised version of the Model 340 was offered to the market in 1979 as the Model 335, later available as the improved Model 335 II version, but production ended in 1980 after only 45 had been built.

1980 Cessna 335
Engine: Continental IO-520-EB, 300 hp@SL to 13,000 ft
TBO (hrs.): 1400
Fuel type: 100/100LL
Propeller type: 3-Blade/constant speed
Landing gear type: Tri./Retr.
Max ramp weight w/VGs (lbs): 6290
Gross weight w/VGs (lbs.): 6290
Landing weight (lbs.) 5990
Empty weight, std. (lbs.): 4240
Useful load, std. (lbs.): 2050
Useful fuel, std (USgals.): 183
Payload, full std. fuel (lbs.): 952
Wingspan: 38 ft. 1 in.
Overall length: 34 ft. 4 in.
Height: 12 ft. 7 in.
Wing area (sq. ft.): 185
Wing loading (lbs./sq.ft.): 32.6
Power loading (lbs./hp): 9.98
Wheel size (in.): 6.00 x 6
Seating capacity: 6
Cabin doors: 1
Cabin width: 46.5 in.
Cabin height: 49 in.   
Cruise speed (kts.) 75% power: 211
Fuel  consumption (USgph.): 75% power: 34
Vso (kts.): 71
Vso w/VGs (kts.): 64
Best rate of climb, SL (fpm): 1400
S/E rate of climb, SL (fpm): 200
Service ceiling (ft.): 26,800
S/E service ceiling (ft.): 11,500
Takeoff ground roll (ft.): 1850
Takeoff over 50-ft. obstacle (ft.): 2365
Landing ground roll (ft.): 770
Landing over 50-ft. obstacle (ft.): 1850